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Proof of Mars Hopper Concept Technologies was an eight-month study funded by ESA’s General Studies Programme from ECSAT in Harwell. The study has focussed on increasing the TRL of key technologies required for the Mars Hopper concept, which were:
- In Situ Resource Utilisation (ISRU) subsystem to collect and store CO2 from the atmosphere and deliver it to the propulsion system. Locally generated propellant doe snot require transportation to Mars providing a huge mass saving
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The Lunar Dust Analysis Package or L-DAP comprises a number of instruments intended to measure the microscopic properties of lunar dust including:
-The size distribution of the lunar dust
-The structure of the dust grains
-The presence and abundance of key components (eg: nanophase Fe)
-The presence and concentration of specific minerals
-The percentage mass of key elements
-The abundance and distribution of H2O, OH and hydrated minerals
-Electrophysical properties and magnetic field and permittivity.
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